N489MC

Service difficulty reports · 217

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE n_number = 'N489MC' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR UIEA2022070700732None · noneM/D SCD FWD O/B DOOR SILL LOWER SKIN FOUND ONE LOCATION CUT OUT CRACK.(<P>CUT OUT AREA REPAIRED AS PER ATLAS AIR EO NO : 4425A500 REV 1.</P>)Sep 10, 2022 · N489MC · Boeing 747 · Cabin Equipment/FurnishingsSDR UIEA2022052800552Doubler · crackedEO 4453A821-1 & 4 FUSELAGE SKIN NOSE WHEEL WELL FORWARD CORNER DOUBLER INSPECTION AND MODIFICATE (SB 747-53A2851) L/H FASTENERS & WASHERS DEVIATIONS DOUBLER S.E.M AND R/H FASTENERS WASHERS DEVIATIONS FASTENER HOLE CRACK (1EA), L/R DOUBLER INSTALLED AS PER BOMay 27, 2022 · N489MC · Boeing 747412F · Fuselage Structure (General)SDR UIEA2022053100560Transmitter · flamed outBTB, ENG 2 TAIL PIPE FIRE OBSERVED BY GROUND OPS. ALL INSPECTIONS C/W TO INCLUDE BSI. VSV AND FUEL FLOW TRANSMITTER REPLACED. T/T HALF TIME LIMIT REPAIR ACCOMPLISHED. MAX POWER ASSURANCE RUNS ACCOMPLISHED.</P>)May 27, 2022 · N489MC · Boeing 747412F · Compressor Bleed GovernorSDR UIEA2022051700485Loop · inoperativeENGINE 2 FIRE DETECTION LOOP A INOP. PLACED ON MDDR 165711 IAW MEL 26-11-02-01, CAT C.May 17, 2022 · N489MC · Boeing 747412F · Detection SystemSDR UIEA2022022000149Eec · failedENGINE #2 FAILED SHORTLY AFTER TAKEOFF (CONVERSATION WITH CAPTAIN INDICATED IFSD ON TAKEOFF AT APPROXIMATELY 1000 AGL. CREW FOLLOWED THE QRH. CREW LEVELED OUT AIRCRAFT AT 3000 FT. CREW INITIATED AN ENGINE START ON #2, WHICH WAS SUCCESSFUL. CREW CONTACTED THE DFeb 20, 2022 · N489MC · Boeing 747412F · Engine (Turbine/Turboprop)SDR UIEA2022012500077None · noneEICAS GEAR TILT(<P ><SPAN>R/H BODY GEAR TILT HYDRAULIC LINE DAMAGED. FABRICATED TEMPORARY REPAIR HOSE FROM FSK PER ATLAS GMM 3.24.1. INSTALLED TEMPORARY REPAIR HOSE PER AMM 32-13-15.</SPAN></P> / <P> </P>)Jan 25, 2022 · N489MC · Boeing 747412F · Main Landing Gear Strut/Axle/TruckSDR UIEA2021092302090Fitting · leakingDURING FLIGHT HYD QTY 1 MSG, FOLLOWED BY HYD SYS 1 MSG AND LIGHT(<P ><SPAN>FOUND FITTINGS ON FUSE ASSY FOR RH BODY GEAR LEAKING. REPLACED RH BODY GEAR TRUCK POSITIONING FUSE IAW AMM 32-13-24/401. LEAK CHECK GOOD.</SPAN></P>)Sep 23, 2021 · N489MC · Boeing 747412F · Main Landing Gear Strut/Axle/TruckSDR UIEA2021081401803Connector · contaminatedIN FLIGHT HYD OVHT #3. IN FLIGHT HYD LOW QTY DOWN TO .12(<P>REMOVED AND REPLACED CANNON PLUG DUE TO MOISTURE AND CONTAMINATION IAW SWPM 20-61-02. REMOVED AND REPLACED #3 HY/DIM CARD (PN <SPAN>D43699J, NSN</SPAN><SPAN>) IAW AMM 29-11-42/401. OPERATIONAL CHECKEAug 13, 2021 · N489MC · Boeing 747412F · Hydraulic Power System WiringSDR UIEA2021072701636Warning Message · multiple failAFTER T/O, #1 PACK INOP. L/H COMM FAILURE, EQUIPMENT COOLING FAILURE, STANDBY INSTRUMENT FAILURE. GENERATED AND EXECUTED E/O 4421A043 FOR DETECTION OF DEFECTS IN A/C SYSTEM.Jul 26, 2021 · N489MC · Boeing 747412F · Central WarningSDR UIEA2021070901501Sensor · faultedEQUIP COOLING MSG ON CLIMB OUT. GRH PERFORMED. ON OVERIDE(<P>PERFORMED FIM 21-58 TASK 833 REMOVED AND REPLACED LOW FLOW SENSOR & EQUIPMENT COOLING CARD (ECC) TEST GOOD IAW AMM 21-58-02 AND 21-58-05/201</P>)Jul 9, 2021 · N489MC · Boeing 747412F · Air Distribution SystemSDR UIEA2020071401515Autothrottle Sys · faultedAUTOTHROTTLE FAULT. DEFERRED PER DDG 22-11-04-02B & 22-31-01, MDDR 131055, CAT 'C'Jul 10, 2020 · N489MC · Boeing 747412F · Auto Throttle SystemSDR UIEA2020070751286Light · no testMAIN DECK L1 DOOR SILL EMERGENCY LIGHT L1853 FAILED OPERATION TESTMAIN DECK L1 DOOR SILL EMERGENCY LIGHT L1853 REPLACED AND TESTED NORMAL AS PER AMM 33-51-05Jul 4, 2020 · N489MC · Boeing 747412F · Emergency LightingSDR UIEA2020070751403Skin · delaminatedLEFT WING OTBD FORE FLAP L/E, FOUND THE OTBD AREA DELAMINATED. THE DELAMINATED AREA WAS REPAIR IAW SRM 51-70-07, PAR 5A, REV 88.Jul 4, 2020 · N489MC · Boeing 747412F · Trailing Edge FlapsSDR UIEA2020070751404Skin · delaminatedLEFT WING OTBD FORE FLAP L/E INBD AREA, FOUND DELAMINATION. PERFORMED A REPAIR IAW SRM 51-70-07, PAR 5A, REV 88.Jul 4, 2020 · N489MC · Boeing 747412F · Trailing Edge FlapsSDR UIEA2020070751405Skin · delaminatedLEFT WING OTBD AFT FLAP T/E AREA, UPPER SURFACE WAS FOUND DELAMINATED. THE DELAMINATED AREA WAS REPAIRED IAW SRM 51-70-07, PAR 5A, REV 88.Jul 4, 2020 · N489MC · Boeing 747412F · Trailing Edge FlapsSDR UIEA2020070761406Skin · delaminatedLEFT WING OTBD MID FLAP T/E AREA UPPER SURFACE WAS FOUND DELAMINATED. PERFORMED A REPAIR IAW SRM 51-70-07, PAR 5A, REV 88.Jul 4, 2020 · N489MC · Boeing 747412F · Trailing Edge FlapsSDR UIEA2020070721412Bracket · damagedFWD CARGO BAY, BS 920 - 940, RBL 60 FLOOR AREA AIR DUCT AFT BRACKET WAS FOUND DAMAGED. THE BRACKET WAS REPLACED IAW RI-21-28-14104, REV A.Jul 4, 2020 · N489MC · Boeing 747412F · Fuselage Main, Attach FittingsSDR UIEA2020070781415Seat Track · corrodedBS 1840, RBL 75, SEAT TRACK FOUND CORRODED. THE CORROSION WAS REMOVED AND THE SEAT TRACK WAS PROTECTED IAW SRM 51-10-02, AND SRM 51-20-01. CHECKED WITHIN LIMITS IAW SRM 53-00-52, ALLOWABLE DAMAGE 1, FIG 101.Jul 4, 2020 · N489MC · Boeing 747412F · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2020070781416Seat Track · corrodedBS 1920, RBL 75, SEAT TRACK WAS FOUND CORRODED. THE CORROSION WAS REMOVED AND THE SEAT TRACK WAS PROTECTED IAW SRM 51-10-02, AND SRM 51-20-0. CHECKED WITHIN LIMITS IAW SRM 53-00-52, ALLOWABLE DAMAGE 1, FIG 101.Jul 4, 2020 · N489MC · Boeing 747412F · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2020070781417Seat Track · corrodedBS 1820, RBL 75, SEAT TRACK FOUND CORRODED. THE CORROSION WAS REMOVED AND THE SEAT TRACK PROTECTED IAW SRM 51-10-02, AND SRM 51-20-01. CHECKED WITHIN LIMITS IAW SRM 53-00-52, ALLOWABLE DAMAGE 1, FIG 101.Jul 4, 2020 · N489MC · Boeing 747412F · Fuselage Structure (General)SDR UIEA2020070721418Structure · corrodedAFT CARGO DOOR INTERNAL LOWER, CENTER AREA HAD TWO AREAS OF CORROSION, THE CORROSION WAS REMOVED AND PROTECTED IAW SRM 52-30-02, AD1, FIG 101.Jul 4, 2020 · N489MC · Boeing 747412F · Cargo/Baggage DoorsSDR UIEA2020070701419Seat Track · corrodedBS 1780, LBL 99 SEAT TRACK WAS FOUND WITH CORROSION. THE SEAT TRACK WAS REPAIRED IAW SRM 53-00-52-2R-6, REPAIR 6, FIG 201.Jul 4, 2020 · N489MC · Boeing 747412F · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2020070721420Seat Track · corrodedBS 1920, LBL 75 SEAT TRACK WAS FOUND WITH CORROSION. THE SEAT TRACK WAS REPAIRED IAW SRM 53-00-52-2R-6, REPAIR 6, FIG 201.Jul 4, 2020 · N489MC · Boeing 747412F · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2020070771426Frame · crackedBS 2598 BULKHEAD RT INNER CHORD AREA, ONE CRACK FOUND ON THE FWD SPLICE FITTING, SECOND LAYER COUNT FROM INBD. APPROX 0.040" IN DEPTH RUNNING AFT AT 4 O`CLOCK POSITION, THE BULKHEAD UPPER CORNER RT SPLICE FITTING WAS REPAIRED IAW RI-53-00-14106 REV A.Jul 4, 2020 · N489MC · Boeing 747412F · Fuselage Main, FrameSDR UIEA2020070791437Skin · delaminatedRIGHT WING INBD MID FLAP INBD L/E, FOUND DELAMINATED. PERFORMED A PERMANENT COMPOSITE REPAIR IAW SRM 51-70-07, PAR 5A, REV 88.Jul 4, 2020 · N489MC · Boeing 747412F · Trailing Edge FlapsSDR UIEA2020070791438Skin · delaminatedRIGHT WING OTBD FORE FLAP L/E, FOUND DELAMINATED FROM INBD 261". PERFORMED A PERMANENT COMPOSITE REPAIR IAW SRM 51-70-07, PAR 5A, REV 88.Jul 4, 2020 · N489MC · Boeing 747412F · Trailing Edge FlapsSDR UIEA2020070791439Skin · delaminatedRIGHT WING INBD FORE FLAP, FWD L/E FOUND DELAMINATED FROM O/B 18". PERFORMED A PERMANENT COMPOSITE REPAIR IAW SRM 51-70-07, PAR 5A, REV 88.Jul 4, 2020 · N489MC · Boeing 747412F · Trailing Edge FlapsSDR UIEA2020070791440Skin · delaminatedRIGHT WING INBD FORE FLAP, FWD L/E WAS FOUND DELAMINATED. PERFORMED A PERMANENT COMPOSITE REPAIR IAW SRM 51-70-07, PAR 5A, REV 88.Jul 4, 2020 · N489MC · Boeing 747412F · Trailing Edge FlapsSDR UIEA2020070791441Skin · dentedRIGHT WING, INBD AFT FLAP LOWER SURFACE, CENTER T/E SECTION WAS FOUND DENTED. PERFORMED A PERMANENT COMPOSITE REPAIR IAW SRM 51-70-07 PAR, 5A REV 88.Jul 4, 2020 · N489MC · Boeing 747412F · Trailing Edge FlapsSDR UIEA2020070762442Skin · delaminatedRIGHT WING OTBD FORE FLAP L/E, FOUND DELAMINATION FROM INBD 339 INCHES. PERFORMED PERMANENT COMPOSITE REPAIR IAW SRM 51-70-07, PAR 5A, REV 88.Jul 4, 2020 · N489MC · Boeing 747412F · Trailing Edge FlapsSDR UIEA2020070791443Skin · delaminatedRIGHT WING OTBD FORE FLAP L/E FROM INBD 46 INCHES HAD DELAMINATION. PERFORMED A PERMANENT COMPOSITE REPAIR IAW SRM 51-70-07, PAR 5A, REV 88.Jul 4, 2020 · N489MC · Boeing 747412F · Trailing Edge FlapsSDR UIEA2020007001444Skin · delaminatedRT WING O/B MID FLAP L/E FOUND DELAM. PERFORMED PERMANENT COMPOSITE REPAIR AS PER SRM 51-70-07 PAR 5A REV 88 AND 'HX' PROCESS CARD CONTROL SEQUENCE NR WKL506740-01 FOR REPAIR DETAILS.Jul 4, 2020 · N489MC · Boeing 747412F · Trailing Edge FlapsSDR UIEA2020070701445Skin · delaminatedRT WING I/B FORE FLAP FWD L/E FOUND DELAM FROM I/B 30". PERFORMED PERMANENT COMPOSITE REPAIR AS PER SRM 51-70-07 PAR 5A REV 88 AND 'HX' PROCESS CARD CONTROL SEQUENCE NR WKL506765-01 FOR REPAIR DETAILS.Jul 4, 2020 · N489MC · Boeing 747412F · Trailing Edge FlapsSDR UIEA2020070701446Skin · delaminatedRT WING O/B FORE FLAP L/E FOUND DELAM FROM I/B 160". PERFORMED PERMANENT COMPOSITE REPAIR AS PER SRM 51-70-07 PAR 5A REV 88 AND 'HX' PROCESS CARD CONTROL SEQUENCE NR WKL506732-01 FOR REPAIR DETAILS.Jul 4, 2020 · N489MC · Boeing 747412F · Trailing Edge FlapsSDR UIEA2020070201470Panel · crackedNR 1 PYLON UPR RUBBER PNL 452TL CRACKED. PERFORMED PERMANENT COMPOSITE REPAIR AS PER 'HX' RI NR RI-54-50-14112 REV A.Jul 4, 2020 · N489MC · Boeing 747412F · Nacelle/Pylon Miscellaneous StructureSDR UIEA2020070701480Access Panel · delaminatedVERT FIN LWR ACCESS PNL 322CL BACK SIDE HONEY CONE FOUND DELAM. PERFORMED METAL HOT BOND REPAIR AS PER "HX" RI NR RI-55-30-14113 REV A.Jul 4, 2020 · N489MC · Boeing 747412F · Vertical Stabilizer, Plate/SkinSDR UIEA2020070701492Bracket · damagedCABIN-STA 1940 LH 20L PDU DISAGREE HANDLE BRACKET FOUND DAMAGED. CABIN-STA 1940 LH 20L PDU DISENGAGE HANDLE BRACKET LOCAL FABRICATED PER RI-25-00-14111 REV A. SUBJECT BRACKET REPLACED AND INSTALLED IAW SRM 51-10-02 AND SRM 51-40-02.Jul 4, 2020 · N489MC · Boeing 747412F · Cabin Equipment/FurnishingsSDR UIEA2020070701493Rib · deformedLT WING I/B AILERON I/B FWD LOWER RIB DEFORMED. LT WING I/B AILERON I/B FWD LOWER RIB PN 65B02206-21 LOCAL FABRICATED IAW DWG AND PL 65B02206-21. SUBJECT BRACKET REPLACED AND INSTALLED IAW SRM 51-10-02 AND SRM 51-40-02.Jul 4, 2020 · N489MC · Boeing 747412F · AileronsSDR UIEA2020070701494Support · crackedBS 2598 B/H LT INNER CHORD AREA 1 EA CRACK FOUND ON THE FRAME SUPPORT (1ST LAYER COUNT FORM I/B) APPROX 1/8" IN DEPTH RUNNING FWD AT POSITION. STA 2598 UPPER CORNER LT FRAME SUPPORT FASTENER HOLE CRACK AREA REPAIRED IAW RI-53-00-14108 REV A AND RI-53-00-14110Jul 4, 2020 · N489MC · Boeing 747412F · Fuselage Miscellaneous StructureSDR UIEA2020070701495Bulkhead · crackedFUSELAGE MAIN FRAME BS 1000 BULKHEAD CHORD STR 37L-STR 39L AFTER INSPECTION FOUND CRACK APPROX 0.75". FUSELAGE MAIN FRAME BS 1000 BULKHEAD CHORD STR 37L- STR 39L CRACKED AREA REPAIRED IAW EO 4453A506 PART 3. THIS REPAIR IS A MAJOR REPAIR.Jul 4, 2020 · N489MC · Boeing 747412F · Fuselage Main, BulkheadSDR UIEA2018082601802Fuse · leakingEICAS 'HYD QTY LOW 1' IN CRUISE, 7:30 INTO FLIGHT. UPON LANDING INTO ANC AIRCRAFT HAD TO BE TOWED OFF OF RUNWAY DUE TO NO NR 1 HYDRAULIC SYSTEM AVAILABLE. INSPECTED AND FOUND LEFT HAND BODY GEAR TRUCK POSITIONING HYDRAULIC FUSE ASSEMBLY LEAKING. SERVICED NR 1 Aug 26, 2018 · N489MC · Boeing 747412F · Hydraulic System, MainSDR UIEA2018070701381Strip · corrodedSTA 990 LOWER END OF THE METAL STRIP ON THE SIDE WALL FOUND CORROSION. CORRODED SIDEWALL METAL STRIP AT STA 990 LOWER END AREA TRIMMED OUT AND SPLICE REPAIR CARRIED OUT IAW EN 1151-118 REV 0.Jul 8, 2018 · N489MC · Boeing 747412F · Fuselage Miscellaneous StructureSDR UIEA2018062801286Tension Tie · crackedATA 53-10, EO 4453A301 PART 5 DURING ACCOMPLISHMENT OF HFEC OPEN HOLE INSPECTION AT STA 840 LT TENSION TIE, FOUND CRACK INDICATION AT FWD AND AFT CHANNEL (TENSION TIE) AT 6 O'CLOCK AND 12 O'CLOCK POSITION. REPAIR ACCOMPLISHED AS PER SB 747-53A2502, FIG 11, REVJul 8, 2018 · N489MC · Boeing 747412F · Fuselage Miscellaneous StructureSDR UIEA2018062901294Seat Track · crackedATA 53-40, MOST O/B SEAT TRACK AT STA 230 FOUND CRACKED. CABIN STA 230 MOST RT O/B CRACK SEAT TRACK REPAIRED AS PER SRM 53-00-52 REPAIR 6 REV 83.Jul 8, 2018 · N489MC · Boeing 747412F · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2018070301328Keelbeam · corrodedATA 53-12, FOUND CORROSION ON KEELBEAM TAPAERED LWR CHORD BETWEEN STA 1030 TO STA 1040 WL 91.0 LBL 9 AS MARKED. CORROSION ON KEELBEAM TAPERED LWR CHORD BETWEEN STA 1032 TO STA 1043 WL 91 LBL 9 REPAIRED AS PER EN 1116-18 REV '-'.Jul 8, 2018 · N489MC · Boeing 747412F · Fuselage Main, KeelSDR UIEA2018070301330Keelbeam · corrodedATA 53-12, FOUND CORROSION ON KEELBEAM TAPERED LWR CHORD AT STA 1058 WL 91.0 LBL 9 AS MARKED. CORROSION ON KEELBEAM TAPERED LWR CHORD AT STA 1063 WL 91 LBL 9 REPAIRED AS PER EN 1116-18 REV ' - '.Jul 8, 2018 · N489MC · Boeing 747412F · Fuselage Main, KeelSDR UIEA2018070301331Keelbeam · corrodedATA 53-12, FOUND CORROSION ON KEELBEAM TAPERED LWR CHORD AT STA 1064 WL 91.0 LBL 9 AS MARKED. CORROSION ON KEELBEAM TAPERED LWR CHORD AT STA 1073 TO STA 1082 REPAIRED AS PER EN 1116-18 REV ' - '.Jul 8, 2018 · N489MC · Boeing 747412F · Fuselage Main, KeelSDR UIEA2018070301332Keelbeam · corrodedATA 53-12, FOUND CORROSION ON KEELBEAM TAPERED LWR CHORD BETWEEN STA 1009 TO STA 1019 WL 91.0 LBL 9 AS MARKED. CORROSION ON KEELBEAM TAPERED LWR CHORD BETWEEN STA 1009 TO STA 1022 WL 91 LBL 9 REPAIRED AS PER EN 1116-18 REV ' - '.Jul 8, 2018 · N489MC · Boeing 747412F · Fuselage Main, KeelSDR UIEA2018070301333Keelbeam · corrodedATA 53-12, FOUND CORROSION ON KEELBEAM TAPERED LWR CHORD BETWEEN STA 999 TO STA 1009 WL 91.0 LBL 9 AS MARKED. CORROSION ON KEELBEAM TAPERED LWR CHORD BETWEEN STA 999 TO STA 1010 WL 91 LBL 9 REPAIRED AS PER EN 1116-18 REV ' - '.Jul 8, 2018 · N489MC · Boeing 747412F · Fuselage Main, KeelSDR UIEA2018070501340Skin · damagedATA 53-30, ALONG STA 740, ALONG S-3L, UPPER CROWN LT FX SKIN AREA FOUND WITH ONE RIVET HOLE ELONGATED. ELONGATED HOLE DAMAGE ON UPPER CROWN FX SKIN AREA AT STA 740 STR S-3L REPAIRED AS PER EN 1129-18 REV ' - '.Jul 8, 2018 · N489MC · Boeing 747412F · Fuselage Main, Plate/Skin
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